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060510s1948 |||a fr||||| |0 0|eng d |
| 080 |
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|a 531.33-255
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| 100 |
1 |
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|a Sibert, Harold W.
|9 283916
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| 245 |
0 |
0 |
|a High-Speed Aerodynamics /
|c Harold W. Sibert.
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| 260 |
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|a New York :
|b Prentice-Hall,
|c 1948.
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| 300 |
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|a 280 p.
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| 490 |
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|a Prentice-Hall Aeronautical Engineering Series
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| 520 |
2 |
|
|a Fundamental relations - Thermodynamical relations - Energy, Bernoulli, and Euler equations - Entropy and isentropic flow - Speed of sound - Mach number - Dynamic and impact pressures - Pressure coefficients - Critical conditions - Standard atmosphere - Altimeter, airspeed indicator, machmeter, and true airspeed meter - Determination of position error - True, indicated, calibrated, and equivalent airspeeds - Aerodynamic heating - Reversible adiabatic flow within a stream-tube - One-dimensional flow in a wind tunnel or nozzle - Partial-derivative equations for compressible flow - Disturbance potential - Ackeret supersonic theory - Flow through a shock wave - Normal shock wave - Supersonic flow past a wedge - Two-dimensional supersonic flow around a corner - Buseman parabolic formula - Supersonic flow past a cone - Adverse effects of high airplane mach numbers - Swept wings and wings of low aspect ratio - Determination of high-speed aerodynamic data - Wing drag from a wake survey - Tables and charts.
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| 599 |
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|a Ubic.:531.33-255 SIB Ej.1 PRES
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| 650 |
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4 |
|a ENERGIA
|9 263384
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| 650 |
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4 |
|a TERMODINAMICA
|9 262699
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| 650 |
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4 |
|a VELOCIDAD DEL SONIDO
|9 283917
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| 650 |
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4 |
|a NUMERO DE MACH
|9 283918
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| 650 |
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4 |
|a ATMOSFERA STANDAR
|9 281616
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| 650 |
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4 |
|a FLUJO EN TUNEL
|9 283919
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| 650 |
|
4 |
|a FLUJO COMPRESIBLE
|9 274615
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| 650 |
|
4 |
|a FLUJO POTENCIAL
|9 274608
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| 650 |
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4 |
|a FLUJO SUPERSONICO
|9 274742
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| 650 |
|
4 |
|a ONDA DE CHOQUE
|9 283687
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| 650 |
|
4 |
|a ALTIMETRO
|9 283920
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| 650 |
|
4 |
|a VELOCIMETRO
|9 278018
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| 650 |
|
4 |
|a VELOCIMETRO
|9 278018
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| 650 |
|
4 |
|a BERNOULLI
|9 283921
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| 650 |
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4 |
|a EULER
|9 283922
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| 942 |
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|c LIB
|6 _
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| 959 |
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|a MON
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| 960 |
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|a 10414
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| 970 |
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|a Registro convertido en forma automatizada
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| 999 |
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|c 9734
|d 9734
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| 040 |
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